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US6986948B2 - Polyester-based dimethacrylates designed for laminating applications - Google Patents

Polyester-based dimethacrylates designed for laminating applications Download PDF

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Publication number
US6986948B2
US6986948B2 US10/274,589 US27458902A US6986948B2 US 6986948 B2 US6986948 B2 US 6986948B2 US 27458902 A US27458902 A US 27458902A US 6986948 B2 US6986948 B2 US 6986948B2
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acid
glycol
alkyl
bis
ply
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US20040076830A1 (en
Inventor
Daniel Joseph Riley
Roman Loza
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Ashland Inc
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Ashland Inc
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Priority to US10/274,589 priority Critical patent/US6986948B2/en
Application filed by Ashland Inc filed Critical Ashland Inc
Priority to MXPA05004214A priority patent/MXPA05004214A/en
Priority to CN2003801061394A priority patent/CN1787911B/en
Priority to EP20030816098 priority patent/EP1560705B1/en
Priority to PCT/US2003/033044 priority patent/WO2004076168A1/en
Priority to AU2003303977A priority patent/AU2003303977A1/en
Priority to CA 2502712 priority patent/CA2502712C/en
Priority to ES03816098T priority patent/ES2386783T3/en
Publication of US20040076830A1 publication Critical patent/US20040076830A1/en
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    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J4/00Adhesives based on organic non-macromolecular compounds having at least one polymerisable carbon-to-carbon unsaturated bond ; adhesives, based on monomers of macromolecular compounds of groups C09J183/00 - C09J183/16
    • C09J4/06Organic non-macromolecular compounds having at least one polymerisable carbon-to-carbon unsaturated bond in combination with a macromolecular compound other than an unsaturated polymer of groups C09J159/00 - C09J187/00
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J167/00Adhesives based on polyesters obtained by reactions forming a carboxylic ester link in the main chain; Adhesives based on derivatives of such polymers
    • C09J167/06Unsaturated polyesters having carbon-to-carbon unsaturation
    • C09J167/07Unsaturated polyesters having carbon-to-carbon unsaturation having terminal carbon-to-carbon unsaturated bonds
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249933Fiber embedded in or on the surface of a natural or synthetic rubber matrix
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249933Fiber embedded in or on the surface of a natural or synthetic rubber matrix
    • Y10T428/249939Two or more layers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994Fiber embedded in or on the surface of a polymeric matrix
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994Fiber embedded in or on the surface of a polymeric matrix
    • Y10T428/24995Two or more layers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/24994Fiber embedded in or on the surface of a polymeric matrix
    • Y10T428/24995Two or more layers
    • Y10T428/249952At least one thermosetting synthetic polymeric material layer
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31511Of epoxy ether
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31511Of epoxy ether
    • Y10T428/31515As intermediate layer
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31786Of polyester [e.g., alkyd, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31786Of polyester [e.g., alkyd, etc.]
    • Y10T428/31797Next to addition polymer from unsaturated monomers

Definitions

  • the parts produced from laminating resins generally are referred to as fiber-reinforced composite parts.
  • the reinforcing fiber includes, inter alia, glass, carbon, polymeric and like fibers.
  • Such fiber-reinforced parts can be made from a variety of materials and by several processes.
  • the processes for making fiber-reinforced composites can be divided into two general types: closed-mold and open-mold processes.
  • closed-mold processes include sheet molding, bulk molding structural reaction injected molding (SRIM), resin transfer molding (RTM), and various vacuum-assisted molding processes. Styrene emissions are of lesser concern in closed molding processes since uncured resin is not exposed to the environment.
  • Open-mold processes are the second general classification of molding processes. Common open-mold processes include spray-up, hand lay-up, rotational molding, filament winding, and the like. In open-mold processes one side of the laminate remains exposed to the environment. Thus, the styrene in the laminating resin can evaporate. Styrene has been classified as a hazardous air pollutant (HAP). Reducing the styrene content of laminating resins is believed to result in lower HAP emissions and a cleaner environment.
  • HAP hazardous air pollutant
  • the laminating resin Since the mold can have uneven surfaces, it is desirable that the laminating resin possesses the ability to fill the resulting voids. Also, it is important that the resin remain uncured and fluid for sufficient time to permit placing of the second layer into contact with the first layer. A resin that hardens too quickly does not permit flexibility in the fabrication process. Thus, the length of time the resin is fluid is measured and is referred to as “gel-time”. After the laminating resin has gelled it is no longer fluid but not hard. Hardening (cure) takes place after the resin has gelled. Usually the part is sufficiently hard so that it can be removed from the mold within 2 to 24 hours of gelation. Hardening times can be shortened by placing the composite parts in an oven maintained at, e.g., 50°-100° C. for, e.g., 1-3 hours. When large parts are being fabricated the use of an oven may not be practical.
  • the laminating resin composition is composed of a polyol that has been end-terminated with an alkyl (meth)acrylate group and diluted with less than about 35 wt-% styrene. Additives are added to the laminating resin composition to adjust shelf-life and gel-time. Additionally, additives are added to harden or cure the resin. In making the laminating resin, unreacted alkyl (meth)acrylate can be reacted with an epoxy to push the reaction to completion.
  • dibasic acids well known in the polyester art include, for example, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebasic acid, dodecanedioic acid, tetrahydrophthalic acid, phthalic acid, isophthalic acid, orthophthalic acid, terephthalic acid, maleic (and fumaric) acid, corresponding anhydrides, and the like, and mixtures thereof.
  • suitable dicarboxylic acids contain from about 4 to 12 carbon atoms.
  • epoxy resins can be used, such as, for example, polyglycidyl ethers of polyhydric polyols, such as ethylene glycol, triethylene glycol, 1,2-propylene glycol, 1,5-pentanediol, 1,2,6-hexanetriol, glycerol, and 2,2-bis(4-hydroxycyclohexyl)propane; polyglycidyl ethers of aliphatic and aromatic polycarboxylic acids, such as, for example, oxalic acid, succinic acid, glutaric acid, terephthalic acid, 2,6-napthalene dicarboxylic acid, and dimerized linoleic acid; polyglycidyl ethers of polyphenols, such as, for example, bis-phenol A, bis-phenol F, 1,1-bis(4-hydroxyphenyl)ethane, 1,1-bis(4-hydroxyphenyl)isobutane, and 1,5-dihydroxy napthalene;
  • methacrylated laminating resins can be used alone to fabricate fiber-reinforced parts, they also can be mixed with other laminating resins to improve performance and/or to enhance their cure.
  • suitable resins that can be mixed with the methacrylated laminating resins include, for example, unsaturated polyester resins (including those made with dicyclopentadiene, DCPD), vinyl ester resins, acrylic resins, polyether resins, polyamine resins, polyamide resins, alkyd resins, and the like and mixtures thereof.
  • Additives incorporated into the methacrylated polyester material are conventional in nature. Accordingly, suitable curing agents, accelerating agents, and the like are incorporated. Pigments, release agents, plasticizers, low shrink additives, surface enhancers, and the like also are used as is necessary, desirable, or convenient in conventional fashion.
  • a bis-phenol A epoxy resin (EPON® 828 difunctional bis-phenol A/epichlorhydrin liquid epoxy resin, 185-192 epoxide equivalent weight, 110-150 poise viscosity @ 25° C., 1.16 g/ml density @ 25° C., Resolution Performance Products, LLC, Houston, Tex.) was added to react with residual (excess and unreacted) methacrylic acid.
  • This adhesive neat is sample 6702-184.
  • Another resin, 6702-187ST was prepared in the same manner with an additional processing step in which volatile components of the resin were removed by vacuum stripping.
  • the two experimental laminating resin blends and the comparative resin blend were promoted and cured using methyl ethyl ketone peroxide (Lupersol DDM-9 available from Elf Atochem North America, Inc. 2000 Market St. Philadelphia, Pa. 19103, labeled as MEK-P in the table). After a post cure the castings were subjected to testing with the results summarized in Table 6 being recorded.
  • methyl ethyl ketone peroxide Liupersol DDM-9 available from Elf Atochem North America, Inc. 2000 Market St. Philadelphia, Pa. 19103, labeled as MEK-P in the table.
  • the laminating resin derived from the methacrylated polyester had a lower viscosity and a lower styrene content relative to the Comparative Example. Additionally, the tensile and flexural properties and water-boil properties of the inventive samples are as good as those of the Comparative resin. The higher HDT of Example 3-B shows that vacuum stripping can be used to improve HDT performance of the laminating resin.
  • polyester polyol prepared by the digestion of poly(ethylene terephthalate) with 2-methyl-1,3-propanediol and trimethylolpropane, TMP, 523 g of methacrylic acid, 106 g of xylene, 2.6 g of triphenyl antimony, 0.33 g of p-benzoquinone, and 6.5 g of p-toluenesulfonic acid monohydrate.
  • the mixture was heated to 121° C. and water of reaction was removed by distillation as a xylene/water azeotrope. During the first 8 hours the water was removed and the xylene was recycled back into the reactor.
  • Bis-phenol A epoxy (312 g, Epon 828) was added to the reaction vessel. The amount of bis-phenol A used was calculated so that the AV would be reduced to about 20. The mixture was heated to 121° C. until the AV had decreased to 21 and the epoxy value to 2.4. The final product had a viscosity of 10,600 cps and could be used for making laminates after addition of about 21% styrene.
  • polyester polyol prepared by condensing, at 202° C. with removal of water, a mixture of tetrahydrophthalic acid, tetrahydrophthalic acid anhydride, neopentyl glycol, 1,6-hexanediol and trimethylol propane, TMP), 622.6 g of methacrylic acid, 114 g of xylene, 3.1 g of triphenyl antimony, 0.36 g of p-benzoquinone, and 7.0 g of p-tolunesulfonic acid monohydrate. The mixture was heated to 121° C.
  • Bis-phenol A epoxy (201 g, Epon 828) was added to the reaction vessel. The amount of bis-phenol A used was calculated so that the AV would be reduced to about 20. The mixture was heated to 121° C. until the AV had decreased to 19 and the epoxy value to 3.6. The final product had a viscosity of 1,220 cps.
  • Example 6 The material of Example 6 (392 g) was diluted with styrene (58 g) and the resulting solution was filtered to remove suspended solids. To the filtered solution were added the following (per 100 g of filtered resin) 0.4 g 6% cobalt NAP-ALL (available from OM Group, Inc., 2301 Scranton Rd., Cleveland, Ohio 44113) 0.1 g of N,N-dimethylanaline (available from Sigma-Aldrich, P.O. Box 2060, Milwaukee, Wis. 53201), 0.03 g BYK® A555 (available from BYK-Chemie, 524 South Cherry St., Wallingford, Conn.
  • NAP-ALL available from OM Group, Inc., 2301 Scranton Rd., Cleveland, Ohio 44113
  • N,N-dimethylanaline available from Sigma-Aldrich, P.O. Box 2060, Milwaukee, Wis. 53201
  • BYK® A555 available from BYK-C
  • This laminating resin had a viscosity of 135 cps and contains about 13% styrene.
  • Laminates prepared from this resin had the following hardness values (top/bottom) after 90 hours: 38/47—2-ply laminate, 40/49—5-ply laminate.

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  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Macromonomer-Based Addition Polymer (AREA)
  • Laminated Bodies (AREA)
  • Polyesters Or Polycarbonates (AREA)

Abstract

A laminate formed from a first fiber-reinforced ply joined by a laminating resin composition to a second fiber-reinforced ply. The laminating resin composition is the cured residue of a polyester resin being end-terminated with an alkyl acrylate group and diluted with less than about 35 wt-% styrene. The first fiber-reinforced ply is laminated to the second fiber-reinforced ply with the laminating resin composition by coating a surface of the first ply with an adhesive composition. The coated first ply surface is joined with a surface of the second ply and the adhesive cured. In making the laminating resin composition, unreacted alkyl acrylate can be reacted with an epoxy to push the reaction to completion.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS
None.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH
Not applicable.
BACKGROUND OF THE INVENTION
The present invention relates generally to laminating resins, such as are used in tub, shower, and marine applications, and more particularly to a laminating resin low in styrene content for low VOC (volatile organic content) formulations.
The amount of styrene necessary to dilute laminating resins, such as unsaturated polyester resins, to an appropriate application viscosity (˜250 cps) is of concern from an environmental and safety viewpoint. Typical laminating resins in this art require between about 35% and 60% styrene. Attempts to address this concern have led to developments that are commercially expensive to implement.
The parts produced from laminating resins generally are referred to as fiber-reinforced composite parts. The reinforcing fiber includes, inter alia, glass, carbon, polymeric and like fibers. Such fiber-reinforced parts can be made from a variety of materials and by several processes. The processes for making fiber-reinforced composites can be divided into two general types: closed-mold and open-mold processes. In a closed-mold process the composite part is fabricated in a manner in which the resin prior to cure is not exposed to the ambient environment. Common closed-mold processes include sheet molding, bulk molding structural reaction injected molding (SRIM), resin transfer molding (RTM), and various vacuum-assisted molding processes. Styrene emissions are of lesser concern in closed molding processes since uncured resin is not exposed to the environment.
Open-mold processes are the second general classification of molding processes. Common open-mold processes include spray-up, hand lay-up, rotational molding, filament winding, and the like. In open-mold processes one side of the laminate remains exposed to the environment. Thus, the styrene in the laminating resin can evaporate. Styrene has been classified as a hazardous air pollutant (HAP). Reducing the styrene content of laminating resins is believed to result in lower HAP emissions and a cleaner environment.
Spray-up is commonly used to fabricate parts using a laminating resin and fiberglass reinforcement. In this process a “chopper-gun” is used. The surface of a mold is sprayed with a mixture of laminating resin and chopped glass fiber. Just prior to application, additives are mixed into the resin to promote hardening (i.e., cure). Once the mold surface is covered with an appropriate amount of glass fiber and resin the surface can be rolled to help entrapped air escape. This step is called “rollout”. Alternatively, mats of woven fiberglass can be used. The laminating resin then is applied to the mat and the surface is rolled to remove entrapped air. In either fashion multiple layers can be built up. These layers can be of the same or different material. Since the mold can have uneven surfaces, it is desirable that the laminating resin possesses the ability to fill the resulting voids. Also, it is important that the resin remain uncured and fluid for sufficient time to permit placing of the second layer into contact with the first layer. A resin that hardens too quickly does not permit flexibility in the fabrication process. Thus, the length of time the resin is fluid is measured and is referred to as “gel-time”. After the laminating resin has gelled it is no longer fluid but not hard. Hardening (cure) takes place after the resin has gelled. Usually the part is sufficiently hard so that it can be removed from the mold within 2 to 24 hours of gelation. Hardening times can be shortened by placing the composite parts in an oven maintained at, e.g., 50°-100° C. for, e.g., 1-3 hours. When large parts are being fabricated the use of an oven may not be practical.
BRIEF SUMMARY OF THE INVENTION
A composite part composed of at least one fiber reinforced ply by combining fiber reinforcement with a laminating resin composition then causing the laminating resin composition to harden (i.e., cure) at ambient or elevated temperature. The laminating resin composition is composed of a polyol that has been end-terminated with an alkyl (meth)acrylate group and diluted with less than about 35 wt-% styrene. Additives are added to the laminating resin composition to adjust shelf-life and gel-time. Additionally, additives are added to harden or cure the resin. In making the laminating resin, unreacted alkyl (meth)acrylate can be reacted with an epoxy to push the reaction to completion.
DETAILED DESCRIPTION OF THE INVENTION
The polyol materials are based on macromolecules with a polyester or polyether backbone. In the polyester polyols, a dibasic acid is condensed with a polyhydridic alcohol or glycol. The diacid can be saturated, aromatic, or contain unsaturation. Polyols based on the reaction product of alkyleneoxides (e.g., ethylene oxide) and bis-phenol A can also be used alone or in combination with the polyester polyol. The polyol, then, is capped with an (meth)acrylate. Cross-linking this acrylated polyester backbone, through the terminal acrylate component, most commonly with styrene, produces a three-dimensional structure. Further information on polyesters can be found, for example, by reference to Kirk-Othmer, Encyclopedia of Chemical Technology, 3d Ed., Vol. 11, pp 129-138, John Wiley & Sons, New York, N.Y. (1982), the disclosure of which is expressly incorporated herein by reference. In addition to (meth)acrylate groups, (alkyl)acrylate groups can be used as the capping agents with alkyl groups ranging from C1 to C8 groups. In keeping with terminology in this field, the parenthetical group is optional. Thus, “(alkyl)acrylate” means “acrylate and alkylacrylate”.
Examples of dibasic acids well known in the polyester art include, for example, glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebasic acid, dodecanedioic acid, tetrahydrophthalic acid, phthalic acid, isophthalic acid, orthophthalic acid, terephthalic acid, maleic (and fumaric) acid, corresponding anhydrides, and the like, and mixtures thereof. Preferably, such suitable dicarboxylic acids contain from about 4 to 12 carbon atoms.
Suitable such glycols include virtually any known difunctional dihydric alcohol, for example, alkylene glycols, typically ranging from about 2 to 8 carbon atoms (including cycloalkylene glycols). Illustrative of such diols are ethylene glycol, 1,3-propanediol, 1,3-butanediol, 1,4-butanediol, 1,5-pentanediol, 1,6-hexanediol, 1,2-propanediol, 1,3-butanediol, 2,3-butanediol, 1,3-pentanediol, 1,2-hexanediol, 3-methyl pentane-1,5-diol, 1,4-cyclohexanedimethanol, neopentylglycol, cyclohexane dimethanol, 2,2,4-trimethyl pentanediol, 2-methyl-1,3-propanediol, bis-phenol A, trimethylol ethane, trimethylol propane, dicyclopentadiene glycol, dibrominepentyl glycol, and the like, and mixtures thereof. Diethylene glycol, polypropylene glycol, dipropylene glycol, triethylene glycol, tripropylene glycol, polyethylene glycol, and the like additionally can be used as necessary, desirable, or convenient.
Generally, the temperature of esterification is maintained in the range of about 150°-230° C. and an esterification catalyst is used. Such catalysts are conventional and include, for example, titanium tetrachloride, zinc acetate, zinc oxide, stannous oxylate, dibutyl tin oxide, and the like. Conventional color stabilizers, e.g., trilauryl phosphite or the like, also can be included in the reaction mixture.
The polyester resin then can be end-capped with methacrylic acid (or anhydride). Broadly, alkylacrylic acids can be used, but for ease in condensing water from the system, methacrylic acid is preferred. A molar excess of methacrylic acid is used with conventional condensation reaction conditions prevailing. Further information on this condensation reaction can be found in Japanese Patents Nos. JP 07007604 and 07103291 and Japanese Patent Applications Nos. 49040329 and 63210143, the disclosures of which are expressly incorporated herein by reference.
At around 80% conversion or so, the condensation reaction can stall. Thus, an epoxide can be added to the reaction mixture to react with unreacted methacrylate monomer to speed up the reaction and carry it to completion, as well as to add additional resinous solids to the ultimate laminating composition. A variety of epoxy resins can be used, such as, for example, polyglycidyl ethers of polyhydric polyols, such as ethylene glycol, triethylene glycol, 1,2-propylene glycol, 1,5-pentanediol, 1,2,6-hexanetriol, glycerol, and 2,2-bis(4-hydroxycyclohexyl)propane; polyglycidyl ethers of aliphatic and aromatic polycarboxylic acids, such as, for example, oxalic acid, succinic acid, glutaric acid, terephthalic acid, 2,6-napthalene dicarboxylic acid, and dimerized linoleic acid; polyglycidyl ethers of polyphenols, such as, for example, bis-phenol A, bis-phenol F, 1,1-bis(4-hydroxyphenyl)ethane, 1,1-bis(4-hydroxyphenyl)isobutane, and 1,5-dihydroxy napthalene; modified epoxy resins with acrylate or urethane moieties; glycidlyamine epoxy resins; and novolak resins; and the like and mixtures thereof.
It should be understood that, while the methacrylated laminating resins can be used alone to fabricate fiber-reinforced parts, they also can be mixed with other laminating resins to improve performance and/or to enhance their cure. Examples of suitable resins that can be mixed with the methacrylated laminating resins include, for example, unsaturated polyester resins (including those made with dicyclopentadiene, DCPD), vinyl ester resins, acrylic resins, polyether resins, polyamine resins, polyamide resins, alkyd resins, and the like and mixtures thereof. Additives incorporated into the methacrylated polyester material are conventional in nature. Accordingly, suitable curing agents, accelerating agents, and the like are incorporated. Pigments, release agents, plasticizers, low shrink additives, surface enhancers, and the like also are used as is necessary, desirable, or convenient in conventional fashion.
Application of the laminating resin composition most often is by spray application techniques. Thus, the viscosity of the methacrylated polyester needs to be suitable therefor. Roller coating application requires yet a different application viscosity. Broadly, application viscosities should be less than about 1000 cps, generally less than about 500 cps, and less than about 250 cps for spray application of the methacrylated polyester.
While the methacrylated polyester will cure over time at ambient temperature, often the laminate will be heated to about 60° to 150° C. for times ranging from about 5 to about 500 minutes. Such heating schedules are practiced at the expense of line speed and energy costs.
While the invention has been described with reference to a preferred embodiment, those skilled in the art will understand that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims. In this application all units are in the metric system and all amounts and percentages are by weight, unless otherwise expressly indicated. Also, all citations referred herein are expressly incorporated herein by reference.
EXAMPLES Example 1 Preparation of Methacrylated Polyester Resin
A 2-liter kettle fitted with a mantel, Vigeroux column, gas inlet, condenser, and Dean Stark trap was charged with the following ingredients:
TABLE 1
Weight Wanted Weight Charged
Ingredient # Ingredient (g) (g)
1 Polyethylene 288.55 288.69
terephthalate polymer
2 2-Methyl-1,3- 283.88 284.00
propanediol
3 Zinc Acetate 0.860 0.8643
4 Hydroquinone (20% 0.215 0.2682
solution in ethylene
glycol/methanol
5 Polyethylene 288.55 289
terephthalate polymer
6 Triphenylantimony 6.85 6.8592
7 MEHQ 1.52 1.5237
8 Methacrylic anhydride 659.17 659.17
9 Methacrylic anhydride 288.60 288.77
The first 4 ingredients were charged into the kettle and heated to 410° F. When the reaction ingredients became homogeneous, ingredient 5 was added and a temperature of 410° F. was maintained until 4 hours after the reaction mixture was homogeneous. The reaction mixture was cooled and Ingredients 6-8 then were charged into the kettle and heated to 235° F. with an air/nitrogen (50/50) sparge, and a condenser was directly connected to the reactor. After 4.5 hours reaction time, Ingredient 9 was added to the reaction mixture and a temperature of 235° F. was maintained for 7 hours. The resin then was exposed to a reduced pressure using a vacuum pump to remove the methacrylic acid. Distillation continued until an acid value of less than 25 was obtained. The final polyester product (6720-24) possessed an acid value of 8.1, a hydroxyl value of 3.6, and 85.4% non-volatiles solids.
Example 2 Testing of Laminating Resin Composition of Example 1
Neat resin castings were prepared from methacrylated polyester of Example 1 at 78.7% nv solids (6720-124-1) and at 85.4% nv solids (6720-124-2) by curing a mixture of the resin and 1% benzoyl peroxide and 0.5% tertiary butyl perbenzoate between two glass plates separated by a ⅛″ silicone rubber gasket. The following cure cycle was used: 160° F. for 2 hours, then 200° F. for 1 hour, then 280° F. for 2 hours.
The castings were tested as follows:
Tensile (ASTM D-638 m MAT-2202)
    • Instron Series IX Automated Tester
    • Sample rate: 5 pts/sec
    • Crosshead speed: 0.2000 in/min
    • 2nd Crosshead speed: 0.000 in/min
    • Full scale load range: 10000 lbf
Heat Distortion Temperature Under Load (ASTM D-648, MAT-2250)
    • Maximum fiber stress: 264 psi
    • Immersion medium: silicone oil
The following results were recorded:
TABLE 2
Tensile Testing Results-Sample 6720-124-1
Max. Elongation Elongation
Tensile at Max. at Thick-
Sample Strength Modulus Load Break Width ness
# (psi) (ksi) (%) (%) (in) (in)
1 8721 474.4 2.34 2.67 0.502 0.110
2 10069 474.6 2.85 3.22 0.514 0.105
3 10951 470.6 3.05 3.67 0.508 0.109
4 10308 470.0 2.99 2.99 0.508 0.107
5 10003 490.2 2/51 3/22 0.507 0.109
Mean 10010 475.9 2.75 0.108 0.503 0.108
SD* 812 8.2 0.31 0.37 0.004 0.002
*SD is standard deviation
TABLE 3
Tensile Testing Results-Sample 6720-124-2
Max. Elongation Elongation
Tensile Modu- at Max. at Thick-
Specimen Strength lus Load Break Width ness
# (psi) (ksi) (%) (%) (in) (in)
1 11592 481.5 3.61 3.61 0.502 0.124
2 10695 489.0 3.02 3.76 0.504 0.125
 3* 9575 451.8 2.58 2.58 0.504 0.123
4 11239 507.9 3.07 3.07 0.506 0.124
5 10759 486.8 3.07 3.73 0.506 0.124
Mean 10759 486.8 3.00 3.35 0.504 0.124
SD 764 22.4 0.40 0.51 0.002 0.001
TABLE 4
HDT Under Load Results
Sample Specimen # Temp (° C.) Temp (° F.)
6720-124-1 1 116.5 241.7
2 115.1 239.2
Mean 115.6 240.4
SD 1.0 1.8
6720-124-2 1 116.1 241.0
2 115.1 239.2
Mean 115.6 240.1
SD 0.7 1.3
TABLE 5
Viscosity at Different Styrene Contents
Viscosity
Sample % Styrene (cps)
6720-124 0 2195
6720-124 10 280
These results demonstrate that this low styrene material has both excellent physical and thermal properties as well as a usable viscosity for spray up applications.
Example 3 Post-reaction of Excess Methacrylic Acid with Epoxy Resin
The condensation reaction between methacrylic acid and a PET-based polyol (PET/2-methyl-1,3-propane diol/neopentyl glycol adduct) was run with an excess of methacrylic acid in toluene solvent with triphenyl antimony, p-benzoquinone, and methane sulfonic acid catalysts. Once esterification had slowed down, the acid catalyst (methane sulfonic acid, MSA) was neutralized with tetramethyl ammonium hydroxide and toluene was removed by distillation. Then, a bis-phenol A epoxy resin (EPON® 828 difunctional bis-phenol A/epichlorhydrin liquid epoxy resin, 185-192 epoxide equivalent weight, 110-150 poise viscosity @ 25° C., 1.16 g/ml density @ 25° C., Resolution Performance Products, LLC, Houston, Tex.) was added to react with residual (excess and unreacted) methacrylic acid. This adhesive neat is sample 6702-184. Another resin, 6702-187ST, was prepared in the same manner with an additional processing step in which volatile components of the resin were removed by vacuum stripping.
These two methacrylate capped laminating resins were blended with an unsaturated polyester resin (AROPOL™ 8014, available from Ashland Chemical, 5200 Blazer Parkway, Dublin, Ohio 43017) and the styrene content was adjusted with styrene to 28% (Example 3-A and 3-B). A comparative laminating resin (3-Comp.) was prepared by mixing AROPOL™ 914 vinyl ester resins (available from Ashland Chemical, 5200 Blazer Parkway, Dublin, Ohio 43017) with the AROPOL™ 8014 and the viscosity was adjusted to 200 cps with styrene. The two experimental laminating resin blends and the comparative resin blend were promoted and cured using methyl ethyl ketone peroxide (Lupersol DDM-9 available from Elf Atochem North America, Inc. 2000 Market St. Philadelphia, Pa. 19103, labeled as MEK-P in the table). After a post cure the castings were subjected to testing with the results summarized in Table 6 being recorded.
TABLE 6
Tensile, Flexural and Water-boil Data for Casting ID
Example
3-Comp. 3-A 3-B
Casting ID (6824-) 75-203 63-209 63-208
Aropol 8014 50% 50% 50%
Aropol 914 50%
6702-184 50%
6702-187ST 50%
Styrene 34% 28% 28%
Viscosity (Brookfield @ 200 148 170
25° C.)
Test Data @ 140° F.
Post Cure
Barcol Hardness 46 47 44
Tensile Strength (psi) 9,431 10,171 10,493
Tensile Modulus (ksi) 514 535 535
Elongation at break 2.22% 2.34% 2.49%
Flexural strength (psi) 17,921 16,534 16,575
Flexural modulus (ksi) 501 514 507
Water @ 212° F. 6-d
Absorption 2.00% 2.16% 1.79%
Extraction −0.08% 0.01% −0.01%
Physical change* 0 1 0
Test data @ 300° F.
Post-Cure
Barcol hardness 48 48 45
HDT (° C.) 111 94 100
*Water-Boil-PC: 0 = no change; 9 = severe attack; on re-dried samples.
The laminating resin derived from the methacrylated polyester had a lower viscosity and a lower styrene content relative to the Comparative Example. Additionally, the tensile and flexural properties and water-boil properties of the inventive samples are as good as those of the Comparative resin. The higher HDT of Example 3-B shows that vacuum stripping can be used to improve HDT performance of the laminating resin.
Example 4 Properties of Polyester-based Dimethacrylates
Additional polyesters were synthesized using various glycols and dibasic acids, and then capped with dimethacrylic acid. The amount of styrene added to the resins was varied. The results recorded are set forth below.
TABLE 7
Polyester Based Dimethacrylates Cured with 1% Benzoyl
Peroxide and 0.5% t-butyl perbenzoate (TBPB)
Tensile Tensile Elon-
Styrene Glycol/ Viscosity Strength Modulus gation HDT
(%) Acid* (cps) (psi) (ksi) (%) (° C.)
6.7 2 EG/P 1800 13784 665 2.70 67.0
16.7 2 EG/P 211 13970 631 3.17 69.5
0 2.2 EG/P 825 10593 786 1.60 75.6
6.0 2.2 EG/P 248 10889 739 1.74 78.2
0 2 DEG/P 594 8483 431 9.71 45.4
5.3 2 DEG/P 248 9221 451 8.11 47.5
0 2.2 EG/I 1430 9296 651 1.50 108
7.9 2.2 EG/I 277 9559 636 2.00 115
0 2 DEG/I 791 11317 516 5.25 50.6
6.6 2 DEG/I 261 11578 544 6.79 53.0
0 1.05 MPdiol/ 2195 10010 476 3.15 116
PET
10 1.05 MPdiol/ 270 10759 487 3.35 116
PET
*EG is ethylene glycol
DEG is diethylene glycol
MPDiol is 2-methyl-1,3-propane diol
P is phthalic acid
I is isophthalic acid
Example 5 Sample 6824-133-101
The following materials were charged to a 2-L reaction vessel: 800 g of polyester polyol prepared by the digestion of poly(ethylene terephthalate) with 2-methyl-1,3-propanediol and trimethylolpropane, TMP, 523 g of methacrylic acid, 106 g of xylene, 2.6 g of triphenyl antimony, 0.33 g of p-benzoquinone, and 6.5 g of p-toluenesulfonic acid monohydrate. The mixture was heated to 121° C. and water of reaction was removed by distillation as a xylene/water azeotrope. During the first 8 hours the water was removed and the xylene was recycled back into the reactor. After 8 hours xylene recycling was discontinued. After 11 hours, the mixture was cooled to 80° C. and 13.8 g of tetramethyl ammonium hydroxide (25% aqueous solution) were added. The mixture was weighed (1,297 g) and the acid value (AV) was measured (92 mg KOH/g).
Bis-phenol A epoxy (312 g, Epon 828) was added to the reaction vessel. The amount of bis-phenol A used was calculated so that the AV would be reduced to about 20. The mixture was heated to 121° C. until the AV had decreased to 21 and the epoxy value to 2.4. The final product had a viscosity of 10,600 cps and could be used for making laminates after addition of about 21% styrene.
Example 6 Sample 6824-144-101
The following materials were charged to a 2-L reaction vessel: 800 g of polyester polyol (prepared by condensing, at 202° C. with removal of water, a mixture of tetrahydrophthalic acid, tetrahydrophthalic acid anhydride, neopentyl glycol, 1,6-hexanediol and trimethylol propane, TMP), 622.6 g of methacrylic acid, 114 g of xylene, 3.1 g of triphenyl antimony, 0.36 g of p-benzoquinone, and 7.0 g of p-tolunesulfonic acid monohydrate. The mixture was heated to 121° C. and water of reaction was removed by distillation as a xylene/water azeotrope. During the first 8 hours the water was removed and the xylene was recycled back into the reactor. After 8 hours, xylene recycling was discontinued. After 11 hours, the mixture was cooled to 80° C. and 14.8 g of tetramethylammonium hydroxide (25% aqueous solution) were added. The mixture was weighed (1,361 g) and the acid value (AV) was measured (64 mg KOH/g).
Bis-phenol A epoxy (201 g, Epon 828) was added to the reaction vessel. The amount of bis-phenol A used was calculated so that the AV would be reduced to about 20. The mixture was heated to 121° C. until the AV had decreased to 19 and the epoxy value to 3.6. The final product had a viscosity of 1,220 cps.
Example 7 Preparation of Laminates from 6824-144-101 (Best Mode)
The material of Example 6 (392 g) was diluted with styrene (58 g) and the resulting solution was filtered to remove suspended solids. To the filtered solution were added the following (per 100 g of filtered resin) 0.4 g 6% cobalt NAP-ALL (available from OM Group, Inc., 2301 Scranton Rd., Cleveland, Ohio 44113) 0.1 g of N,N-dimethylanaline (available from Sigma-Aldrich, P.O. Box 2060, Milwaukee, Wis. 53201), 0.03 g BYK® A555 (available from BYK-Chemie, 524 South Cherry St., Wallingford, Conn. 06492) and 0.08 g of a 10% solution of hydroquinone in propylene glycol to prepare a laminating resin. This laminating resin had a viscosity of 135 cps and contains about 13% styrene.
Lupersol DDM-9 (1.8 g) curative was added to a 120 g sample of the laminating resin and was used to make a 2-ply and a 5-ply laminate (with 1.5 oz chopped-glass mat as the reinforcement). The laminates were allowed to cure at room temperature for 90 hours and then the Barcol hardness was measured. Harness values (top/bottom) were as follows: 41/47—2-ply laminate, 47/53—5-ply laminate. These results compare favorably with data obtained using a conventional unsaturated polyester resin (UPR). However, the conventional UPR had a styrene content of 46% and a viscosity of 266 cps. Laminates prepared from this resin had the following hardness values (top/bottom) after 90 hours: 38/47—2-ply laminate, 40/49—5-ply laminate. These results show that the methacrylated polyester resins can be used to make laminates that cure well at ambient conditions but contain considerably less styrene than conventional UPR laminating resins.

Claims (20)

1. A laminate ply formed from a first fiber-reinforcement joined by a laminating resin composition, said laminating resin composition comprising the cured residue of:
one or more of a saturated or aromatic polyester resin being end-terminated by esterification with one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride and diluted with less than about 35 wt-% styrene to spray application viscosity of less than about 500 cps.
2. The laminate ply of claim 1, wherein said one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride is one or more of methacrylic acid or methacrylic anhydride.
3. The laminate of ply claim 1, wherein said alkyl groups of said one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride range from C1 to C8 groups.
4. The laminate of ply claim 1, wherein said polyester resin is formulated from a dibasic acid being one or more of glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebasic acid, dodecanedioic acid, tetrahydrophthalic acid, phthalic acid, isophthalic acid, orthophthalic acid, terephthalic acid, or their corresponding anhydrides; and a glycol being one or more of ethylene glycol, 1,3-propanediol, 1,3-butanediol, 1,4-butanediol, 1,5-pentanediol, 1,6-hexanediol, 1,2-propanediol, 2,3-butanediol, 1,3-pentanediol, 1,2-hexanediol, 2-methyl-1,3-propanediol, 3-methyl pentane-1,5-diol, 1,4-cyclohexanedimethanol, neopentylglycol, cyclohexane dimethanol, 2,2,4-trimethyl pentanediol, bis-phenol A, trimethylol ethane, trimethylol propane, dicyclopentadiene glycol, dibrominepentyl glycol, diethylene glycol, polypropylene glycol, dipropylene glycol, triethylene glycol, or tripropylene glycol, polyethylene glycol.
5. The laminate ply of claim 1, wherein end-terminated polyester resin is further reacted with an epoxide to react with unreacted one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride to speed up the reaction and carry it to completion.
6. The laminate ply of claim 5, wherein said epoxide is one or more of glycidyl ethers of ethylene glycol, triethylene glycol, 1,2-propylene glycol, 1,5-pentanediol, 1,2,6-hexanetriol, glycerol, and 2,2-bis(4-hydroxycyclohexyl)propane; polyglycidyl ethers of oxalic acid, succinic acid, glutaric acid, terephthalic acid, 2,6-napthalene dicarboxylic acid, and dimerized linoleic acid; glycidyl ethers of bis-phenol A, bis-phenol F, 1,1-bis(4-hydroxyphenyl)ethane, 1,1-bis(4-hydroxyphenyl)isobutane, 1,5-dihydroxy napthalene; modified epoxy resins with acrylate or urethane moieties; glycidlyamine epoxy resins; poly(bisphenol A-co-epichlorhydrin); or glycidyl ethers of novolak resins.
7. The laminate ply of claim 1, wherein said first fiber reinforcement is one or more of glass, carbon, a polymeric fiber.
8. A laminate formed from a first fiber-reinforced ply joined by a laminating resin composition to a second fiber-reinforced ply, said laminating resin composition comprising the cured residue of:
one or more of a saturated or aromatic polyester resin being end-terminated by esterification with one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride end diluted with less than about 35 wt-% styrene to spray application viscosity of less than about 500 cps.
9. The laminate of claim 8, wherein said one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride is one or more of methacrylic acid or methacrylic anhydride.
10. The laminate of claim 8, wherein said alkyl groups of said one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride range from C1 to C8 groups.
11. The laminate of claim 8, wherein said polyester resin is formulated from a dibasic acid being one or more of glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebasic acid, dodecanedioic acid, tetrahydrophthalic acid, phthalic acid, isophthalic acid, orthophthalic acid, terephthalic acid, or their corresponding anhydrides; and a glycol being one or more of ethylene glycol, 1,3-propanediol, 1,3-butanediol, 1,4-butanediol, 1,5-pentanediol, 1,6-hexanediol, 1,2-propanediol, 2,3-butanediol, 1,3-pentanediol, 1,2-hexanediol, 2-methyl-1,3-propanediol, 3-methyl pentane-1,5-diol, 1,4-cyclohexanedimethanol, neopentylglycol, cyclohexane dimethanol, 2,2,4-trimethyl pentanediol, bis-phenol A, trimethylol ethane, trimethylol propane, dicyclopentadiene glycol, dibrominepentyl glycol, diethylene glycol, polypropylene glycol, dipropylene glycol, triethylene glycol, or tripropylene glycol, polyethylene glycol.
12. The laminate of claim 8, wherein end-terminated polyester resin is further reacted with an epoxide to react with unreacted one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride to speed up the reaction and carry it to completion.
13. The laminate of claim 12, wherein said epoxide is one or more of glycidyl ethers of ethylene glycol, triethylene glycol, 1,2-propylene glycol, 1,5-pentanediol, 1,2,6-hexanetriol, glycerol, and 2,2-bis(4-hydroxycyclohexyl)propane; polyglycidyl ethers of oxalic acid, succinic acid, glutaric acid, terephthalic acid, 2,6-napthalene dicarboxylic acid, and dimerized linoleic acid; glycidyl ethers of bis-phenol A, bis-phenol F, 1,1-bis(4-hydroxyphenyl)ethane, 1,1-bis(4-hydroxyphenyl)isobutane, 1,5-dihydroxy napthalene; modified epoxy resins with acrylate or urethane moieties; glycidlyamine epoxy resins; poly(bisphenol A-co-epichlorohydrin); or glycidyl ethers of novolak resins.
14. The laminate or claim 8, wherein said first fiber reinforcement is one or more of glass, carbon, a poylymeric fiber.
15. A method for laminating first fiber-reinforced ply joined to a second fiber-reinforced ply with a laminating resin composition, which comprises the steps of:
(a) coating a surface of said first ply with a laminating resin composition comprising one or more of a saturated or aromatic polyester resin being end-terminated by esterification with one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride and diluted with less than about 35 wt-% styrene to spray application viscosity of less than about 500 cps; and
(b) joining said coated first ply surface with a surface of said second ply; and
(c) curing said adhesive.
16. The method of claim 15, wherein said one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride is one or more of methacrylic acid or methacrylic anhydride.
17. The method of claim 15, wherein said polyester resin is formulated from a dibasic acid being one or more of glutaric acid, adipic acid, pimelic acid, suberic acid, azelaic acid, sebasic acid, dodecanedioic acid, tetrahydrophthalic acid, phthalic acid, isophthalic acid, orthophthalic acid, terephthalic acid, or their corresponding anhydrides; and a glycol being one or more of ethylene glycol, 1,3-propanediol, 1,3-butanediol, 1,4-butanediol, 1,5-pentanediol, 1,6-hexanediol, 1,2-propanediol, 2,3-butanediol, 1,3-pentanediol, 1,2-hexanediol, 2-methyl-1,3-propanediol, 3-methyl pentane-1,5-diol, 1,4-cyclohexanedimethanol, neopentylglycol, cyclohexane dimethanol, 2,2,4-trimethyl pentanediol, bis-phenol A, trimethylol ethane, trimethylol propane, dicyclopentadiene glycol, dibrominepentyl glycol, diethylene glycol, polypropylene glycol, dipropylene glycol, triethylene glycol, or tripropylene glycol, polyethylene glycol.
18. The method of claim 15, wherein end-terminated polyester resin is further reacted with an epoxide to react with unreacted one or more of an (alkyl)acrylic acid or an (alkyl)acrylic acid anhydride to speed up the reaction and carry it to completion.
19. The laminate of claim 12, wherein said epoxide is one or more of glycidyl ethers of ethylene glycol, triethylene glycol, 1,2-propylene glycol, 1,5-pentanediol, 1,2,6-hexanetriol, glycerol, and 2,2-bis(4-hydroxycyclohexyl)propane; polyglycidyl ethers of oxalic acid, succinic acid, glutaric acid, terephthalic acid, 2,6-napthalene dicarboxylic acid, and dimerized linoleic acid; glycidyl ethers of bis-phenol A, bis-phenol F, 1,1-bis(4-hydroxyphenyl)ethane, 1,1-bis(4-hydroxyphenyl)isobutane, 1,5-dihydroxy napthalene; modified epoxy resins with acrylate or urethane moieties; glycidlyamine epoxy resins; poly(bisphenol A-co-epichlorohydrin); or glycidyl ethers of novolak resins.
20. The method of claim 15, wherein said first fiber reinforcement is one or more of glass, carbon, a poylymeric fiber.
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ES2386783T3 (en) 2012-08-30
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EP1560705A4 (en) 2011-05-11
MXPA05004214A (en) 2005-07-13
CN1787911A (en) 2006-06-14
EP1560705A1 (en) 2005-08-10
EP1560705B1 (en) 2012-06-06
AU2003303977A1 (en) 2004-09-17
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US20040076830A1 (en) 2004-04-22
CA2502712C (en) 2010-07-06

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